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Engine Model: SEPR 740. Manufacturer Name: SEPR 740. Designer: SEPR. Developed in: 1962. Gross Mass: 1,050 kg (2,310 lb). Empty Mass: 310 kg (680 lb). Propellants: Solid. Thrust(vac): 91.700 kN (20,615 lbf). Isp: 230 sec. Burn time: 18 sec. Diameter: 0.57 m (1.87 ft). Length: 3.20 m (10.40 ft). Chambers: 1. Country: France. Status: Out of production. First Flight: 1962.
Engine Model: SEPR 740-3. Designer: ONERA. Gross Mass: 1,100 kg (2,400 lb). Empty Mass: 372 kg (820 lb). Propellants: Solid. Thrust(vac): 170.000 kN (38,210 lbf). Burn time: 20 sec. Diameter: 0.56 m (1.83 ft). Length: 3.80 m (12.40 ft). Country: France.
SEPR 740 used on Rocket Stages
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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